WO2013028164A8 - Tangential annular combustor with premixed fuel and air for use on gas turbine engines - Google Patents
Tangential annular combustor with premixed fuel and air for use on gas turbine engines Download PDFInfo
- Publication number
- WO2013028164A8 WO2013028164A8 PCT/US2011/048595 US2011048595W WO2013028164A8 WO 2013028164 A8 WO2013028164 A8 WO 2013028164A8 US 2011048595 W US2011048595 W US 2011048595W WO 2013028164 A8 WO2013028164 A8 WO 2013028164A8
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- air
- fuel
- combustion
- gas turbine
- turbine engines
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/58—Cyclone or vortex type combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/128—Nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03041—Effusion cooled combustion chamber walls or domes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03045—Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
- Y02T50/678—Aviation using fuels of non-fossil origin
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014527125A JP6110854B2 (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel air for use in gas turbine engines |
PCT/US2011/048595 WO2013028164A2 (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
EP11871342.9A EP2748533A4 (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
KR1020147007517A KR101774630B1 (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
CN201180073012.1A CN103930723A (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
RU2014110629A RU2626887C2 (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2011/048595 WO2013028164A2 (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
Publications (3)
Publication Number | Publication Date |
---|---|
WO2013028164A2 WO2013028164A2 (en) | 2013-02-28 |
WO2013028164A3 WO2013028164A3 (en) | 2014-03-20 |
WO2013028164A8 true WO2013028164A8 (en) | 2014-04-10 |
Family
ID=47747017
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2011/048595 WO2013028164A2 (en) | 2011-08-22 | 2011-08-22 | Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP2748533A4 (en) |
JP (1) | JP6110854B2 (en) |
KR (1) | KR101774630B1 (en) |
CN (1) | CN103930723A (en) |
RU (1) | RU2626887C2 (en) |
WO (1) | WO2013028164A2 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013028163A1 (en) * | 2011-08-22 | 2013-02-28 | Majed Toqan | Tangential and flameless annular combustor for use on gas turbine engines |
CN104180398A (en) * | 2014-08-24 | 2014-12-03 | 武汉英康汇通电气有限公司 | Annular combustor |
CN104949154B (en) * | 2015-03-11 | 2017-10-31 | 龚雨晋 | Realize the device of constant volume burning and the dynamical system including the device |
US11378277B2 (en) | 2018-04-06 | 2022-07-05 | General Electric Company | Gas turbine engine and combustor having air inlets and pilot burner |
CN108826357A (en) * | 2018-07-27 | 2018-11-16 | 清华大学 | The toroidal combustion chamber of engine |
CN110081429B (en) * | 2019-05-31 | 2024-04-12 | 南方电网电力科技股份有限公司 | Sludge and garbage mixing incineration method and device |
US11035298B1 (en) * | 2020-03-16 | 2021-06-15 | Heleng Inc. | Turbine engine system |
US11448175B1 (en) * | 2021-06-03 | 2022-09-20 | General Electric Company | Fuel nozzle |
KR102583222B1 (en) | 2022-01-06 | 2023-09-25 | 두산에너빌리티 주식회사 | Nozzle for combustor, combustor, and gas turbine including the same |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3433015A (en) * | 1965-06-23 | 1969-03-18 | Nasa | Gas turbine combustion apparatus |
US4216652A (en) * | 1978-06-08 | 1980-08-12 | General Motors Corporation | Integrated, replaceable combustor swirler and fuel injector |
US4891936A (en) * | 1987-12-28 | 1990-01-09 | Sundstrand Corporation | Turbine combustor with tangential fuel injection and bender jets |
SU1575010A1 (en) * | 1988-05-17 | 1990-06-30 | Производственное объединение "Невский завод" им.В.И.Ленина | Composition chamber of gas-turbine unit |
US5113647A (en) * | 1989-12-22 | 1992-05-19 | Sundstrand Corporation | Gas turbine annular combustor |
US5177955A (en) * | 1991-02-07 | 1993-01-12 | Sundstrand Corp. | Dual zone single manifold fuel injection system |
US5669218A (en) * | 1995-05-31 | 1997-09-23 | Dresser-Rand Company | Premix fuel nozzle |
US6453658B1 (en) * | 2000-02-24 | 2002-09-24 | Capstone Turbine Corporation | Multi-stage multi-plane combustion system for a gas turbine engine |
US6397603B1 (en) * | 2000-05-05 | 2002-06-04 | The United States Of America As Represented By The Secretary Of The Air Force | Conbustor having a ceramic matrix composite liner |
US6655146B2 (en) * | 2001-07-31 | 2003-12-02 | General Electric Company | Hybrid film cooled combustor liner |
US6751961B2 (en) * | 2002-05-14 | 2004-06-22 | United Technologies Corporation | Bulkhead panel for use in a combustion chamber of a gas turbine engine |
US7052231B2 (en) * | 2003-04-28 | 2006-05-30 | General Electric Company | Methods and apparatus for injecting fluids in gas turbine engines |
US20070107437A1 (en) * | 2005-11-15 | 2007-05-17 | Evulet Andrei T | Low emission combustion and method of operation |
US7665307B2 (en) * | 2005-12-22 | 2010-02-23 | United Technologies Corporation | Dual wall combustor liner |
US8015814B2 (en) * | 2006-10-24 | 2011-09-13 | Caterpillar Inc. | Turbine engine having folded annular jet combustor |
FR2917487B1 (en) * | 2007-06-14 | 2009-10-02 | Snecma Sa | TURBOMACHINE COMBUSTION CHAMBER WITH HELICOIDAL CIRCULATION OF THE AIR |
US20090133854A1 (en) * | 2007-11-27 | 2009-05-28 | Bruce Carlyle Johnson | Flameless thermal oxidation apparatus and methods |
US20100192582A1 (en) * | 2009-02-04 | 2010-08-05 | Robert Bland | Combustor nozzle |
US8234872B2 (en) * | 2009-05-01 | 2012-08-07 | General Electric Company | Turbine air flow conditioner |
US8904799B2 (en) * | 2009-05-25 | 2014-12-09 | Majed Toqan | Tangential combustor with vaneless turbine for use on gas turbine engines |
US8388307B2 (en) * | 2009-07-21 | 2013-03-05 | Honeywell International Inc. | Turbine nozzle assembly including radially-compliant spring member for gas turbine engine |
-
2011
- 2011-08-22 EP EP11871342.9A patent/EP2748533A4/en not_active Withdrawn
- 2011-08-22 CN CN201180073012.1A patent/CN103930723A/en active Pending
- 2011-08-22 WO PCT/US2011/048595 patent/WO2013028164A2/en active Application Filing
- 2011-08-22 JP JP2014527125A patent/JP6110854B2/en active Active
- 2011-08-22 KR KR1020147007517A patent/KR101774630B1/en active IP Right Grant
- 2011-08-22 RU RU2014110629A patent/RU2626887C2/en active
Also Published As
Publication number | Publication date |
---|---|
RU2014110629A (en) | 2015-09-27 |
JP6110854B2 (en) | 2017-04-05 |
RU2626887C2 (en) | 2017-08-02 |
KR101774630B1 (en) | 2017-09-19 |
KR20140090141A (en) | 2014-07-16 |
CN103930723A (en) | 2014-07-16 |
WO2013028164A2 (en) | 2013-02-28 |
JP2014524562A (en) | 2014-09-22 |
EP2748533A2 (en) | 2014-07-02 |
EP2748533A4 (en) | 2015-03-04 |
WO2013028164A3 (en) | 2014-03-20 |
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